Airworthiness Directives; SOCATA-Groupe AEROSPATIALE Model TBM 700 Airplanes
airworthiness · Rule · Final rule. · Published 2002-05-07 · Effective 2002-06-20 · 67 FR 30541
Document
Document number
02-11215
Federal Register citation
67 FR 30541
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
SOCATA-Groupe AEROSPATIALE Model TBM 700
Publication date
2002-05-07
Effective date
2002-06-20
FAA docket
Docket No. 2002-CE-01-AD
Abstract
This amendment supersedes Airworthiness Directive (AD) 2001- 05-03, which applies to certain SOCATA--Groupe AEROSPATIALE (Socata) Model TBM 700 airplanes. AD 2001-05-03 currently requires you to apply Loctite on attaching bolt/screw threads of inboard, central, and outboard carriages; increase tightening torques of associated hardware; and replace central carriage attaching bolts. The French airworthiness authority has determined that certain service information referenced in AD 2001-05-03 be removed and additional inspection of the flap carriage attaching bolts, screws, and barrel nut be included. Therefore, this AD will retain the requirements of the current AD and will add the information communicated by the French airworthiness authority. The actions specified by this AD are intended to prevent the flap attaching bolts/screws from becoming loose and separating from the airplane, which could cause rough or irregular control. Such rough or irregular control could lead to the loss of control of the airplane.